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Space Shuttle, Orion, Apollo CSM: Active Upper ... Saturn V: 1st RP-1 / ... 5.97: Space Shuttle Solid Rocket Booster [k]
The Saturn-Shuttle was a preliminary concept of launching the Space Shuttle orbiter using a modified version of the first stage of the Saturn V rocket. [1] It was studied and considered in 1971–1972.
Comparison of Saturn V, Shuttle, Ares I, Ares V, Ares IV, and SLS Block 1. U.S. proposals for a rocket larger than the Saturn V from the late 1950s through the early 1980s were generally called Nova. Over thirty different large rocket proposals carried the Nova name, but none were developed. [93]
TLON Space 10 m 25: N/A N/A N/A Launch platform 2025 Blue Whale 1 South Korea: Perigee Aerospace: 21 m 165 [152] N/A 185 to SSO Partially reusable: CETACEA 1 sea launch platform [153] Esrange: 2024 [154] 195 [152] 220 to SSO Expendable: Cosmos Russia: SR space: 18.5 m 390: N/A 310 to SSO N/A Vostochny, Yasny: TBA Cyclone-4M Ukraine: Yuzhnoye ...
The American Saturn MLV family of rockets was proposed in 1965 by NASA as successors to the Saturn V rocket. [64] It would have been able to carry up to 160,880 kg (354,680 lb) to low Earth orbit. The Nova designs were also studied by NASA before the agency chose the Saturn V in the early 1960s [65] Nova was cancelled in 1964 and had reusable ...
Saturn IB Saturn V: 3: 8.5: 3.91: 5,500 CM + 14,700 LM + 24,500 Service Module: Fuel cells Parachute splashdown (two drogues, three pilots, three mains) 1967 (1966) 1975: 15 (4) [note 3] Space Shuttle orbiter USA: Rockwell International: LEO: Space Shuttle: 8 [note 4] 37.24: 4.8 [note 5] 109,000: Fuel cells Runway landing (with one pilot and ...
A Saturn V rocket, one of the most powerful operational launch vehicles to date. This article compares different orbital launcher families (launchers which are significantly different from other members of the same 'family' have separate entries).
The use of mobile launcher platform is a part of the Integrate-Transfer-Launch (ITL) system, which involves vertical assembly, transport, and launch of rockets. The concept was first implemented in the 1960s for the United States Air Force's Titan III rocket, and it was later used by NASA for Saturn V, Space Shuttle, and Space Launch System. [1]
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